Acta Metallurgica Sinica (English Letters) ›› 2019, Vol. 32 ›› Issue (6): 684-694.DOI: 10.1007/s40195-018-00869-w
Special Issue: 2019年铝合金专辑; 2018-2019焊接专辑
• Orginal Article • Previous Articles Next Articles
Deng-Kui Zhang1, Guo-Qing Wang2(), Ai-Ping Wu1,3,4(
), Ji-Guo Shan1,4, Yue Zhao1,4, Tian-Yi Zhao1, Dan-Yang Meng5, Jian-Ling Song5, Zhong-Ping Zhang5
Received:
2018-08-04
Revised:
2018-11-05
Online:
2019-06-10
Published:
2019-06-17
Supported by:
Deng-Kui Zhang, Guo-Qing Wang, Ai-Ping Wu, Ji-Guo Shan, Yue Zhao, Tian-Yi Zhao, Dan-Yang Meng, Jian-Ling Song, Zhong-Ping Zhang. Effects of Post-weld Heat Treatment on Microstructure, Mechanical Properties and the Role of Weld Reinforcement in 2219 Aluminum Alloy TIG-Welded Joints[J]. Acta Metallurgica Sinica (English Letters), 2019, 32(6): 684-694.
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Alloy | Si | Fe | Cu | Mn | Mg | Zn | Ti | Zr | V | Al |
---|---|---|---|---|---|---|---|---|---|---|
2219 | 0.2 | 0.3 | 5.8-6.8 | 0.2-0.4 | 0.02 | 0.1 | 0.02-0.10 | 0.10-0.25 | 0.05-0.15 | Bal. |
2325 | - | - | 6.0-6.8 | 0.2-0.4 | - | - | 0.1-0.2 | - | - | Bal. |
Table 1 Chemical compositions of 2219 aluminum alloy and ER2325 filler metal (wt.%)
Alloy | Si | Fe | Cu | Mn | Mg | Zn | Ti | Zr | V | Al |
---|---|---|---|---|---|---|---|---|---|---|
2219 | 0.2 | 0.3 | 5.8-6.8 | 0.2-0.4 | 0.02 | 0.1 | 0.02-0.10 | 0.10-0.25 | 0.05-0.15 | Bal. |
2325 | - | - | 6.0-6.8 | 0.2-0.4 | - | - | 0.1-0.2 | - | - | Bal. |
Butt-welded plate joint | Welding layer | Welding heat input, η (J·cm-1) | Wire feeding speed (mm·min-1) |
---|---|---|---|
1# | First layer | 12,825 | - |
Second layer | 29,314 | 600 | |
Thirdlayer | 37,620 | 800 | |
2# | First layer | 12,825 | - |
Second layer | 29,314 | 400 | |
Third layer | 33,094 | 800 |
Table 2 Welding process parameters of the two butt-welded plate joints (η represents the power factor of the arc)
Butt-welded plate joint | Welding layer | Welding heat input, η (J·cm-1) | Wire feeding speed (mm·min-1) |
---|---|---|---|
1# | First layer | 12,825 | - |
Second layer | 29,314 | 600 | |
Thirdlayer | 37,620 | 800 | |
2# | First layer | 12,825 | - |
Second layer | 29,314 | 400 | |
Third layer | 33,094 | 800 |
Fig. 3 TEM images of 2219-C10S aluminum alloy: a-c the microstructure of the different phase, respectively; d, e the selected area diffraction pattern from a, b, respectively
Fig. 4 Microstructure of WZ before and after the post-weld heat treatment: a1, a2, b1, b2, c1, c2 the upper, the middle and the lower layer of the WZ in as-welded state; d1, d2, e1, e2, f1, f2 the upper, the middle and the lower layer of the WZ after the post-weld heat treatment
No. | A 1 | A 2 | A 3 | B 1 | B 2 | B 3 | C 1 | C 2 | C 3 |
---|---|---|---|---|---|---|---|---|---|
Cu | 3.19 | 3.57 | 2.84 | 3.91 | 4.02 | 3.85 | 2.17 | 2.46 | 2.44 |
Average: 3.20 | Average: 3.93 | Average: 2.36 | |||||||
Al | 96.81 | 96.43 | 97.16 | 96.09 | 95.98 | 96.15 | 97.83 | 97.54 | 97.56 |
Average: 96.80 | Average: 96.07 | Average: 97.64 | |||||||
No. | D 1 | D 2 | D 3 | E 1 | E 2 | E 3 | F 1 | F 2 | F 3 |
Cu | 7.83 | 7.51 | 7.64 | 7.88 | 7.77 | 8.61 | 7.72 | 7.81 | 7.79 |
Average: 7.66 | Average: 8.09 | Average: 7.77 | |||||||
Al | 92.17 | 92.49 | 92.36 | 92.12 | 92.23 | 91.39 | 92.28 | 92.19 | 92.21 |
Average: 92.34 | Average: 91.91 | Average: 92.23 |
Table 3 EDS analysis results of the α-Al matrix in Fig. 4 (wt.%)
No. | A 1 | A 2 | A 3 | B 1 | B 2 | B 3 | C 1 | C 2 | C 3 |
---|---|---|---|---|---|---|---|---|---|
Cu | 3.19 | 3.57 | 2.84 | 3.91 | 4.02 | 3.85 | 2.17 | 2.46 | 2.44 |
Average: 3.20 | Average: 3.93 | Average: 2.36 | |||||||
Al | 96.81 | 96.43 | 97.16 | 96.09 | 95.98 | 96.15 | 97.83 | 97.54 | 97.56 |
Average: 96.80 | Average: 96.07 | Average: 97.64 | |||||||
No. | D 1 | D 2 | D 3 | E 1 | E 2 | E 3 | F 1 | F 2 | F 3 |
Cu | 7.83 | 7.51 | 7.64 | 7.88 | 7.77 | 8.61 | 7.72 | 7.81 | 7.79 |
Average: 7.66 | Average: 8.09 | Average: 7.77 | |||||||
Al | 92.17 | 92.49 | 92.36 | 92.12 | 92.23 | 91.39 | 92.28 | 92.19 | 92.21 |
Average: 92.34 | Average: 91.91 | Average: 92.23 |
Fig. 5 Microstructure of joint’s PMZ, OAZ, HAZ before and after the post-weld heat treatment: a1, a2, b1, b2, c1, c2 the region of PMZ, OAZ and HAZ in as-welded state; d1, d2, e1, e2, f1, f2 the region of PMZ, OAZ and HAZ after the post-weld heat treatment
No. | A 1 | A 2 | A 3 | B 1 | B 2 | B 3 | C 1 | C 2 | C 3 |
---|---|---|---|---|---|---|---|---|---|
Cu | 7.91 | 8.04 | 7.93 | 7.73 | 7.67 | 7.94 | 7.96 | 7.44 | 7.79 |
Average: 7.96 | Average: 7.78 | Average: 7.73 | |||||||
Al | 92.09 | 91.96 | 92.07 | 92.27 | 92.33 | 92.06 | 92.04 | 92.56 | 92.22 |
Average: 92.04 | Average: 92.22 | Average: 92.27 |
Table 4 EDS analysis results of the α-Al matrix in Fig. 5 (wt.%)
No. | A 1 | A 2 | A 3 | B 1 | B 2 | B 3 | C 1 | C 2 | C 3 |
---|---|---|---|---|---|---|---|---|---|
Cu | 7.91 | 8.04 | 7.93 | 7.73 | 7.67 | 7.94 | 7.96 | 7.44 | 7.79 |
Average: 7.96 | Average: 7.78 | Average: 7.73 | |||||||
Al | 92.09 | 91.96 | 92.07 | 92.27 | 92.33 | 92.06 | 92.04 | 92.56 | 92.22 |
Average: 92.04 | Average: 92.22 | Average: 92.27 |
Fig. 6 Microhardness distribution on transverse cross section of the joints: a, b the locations of hardness testing of 1# and 2# joints; c, d the hardness distribution of 1# joint before and after the post-weld heat treatment; e, f the hardness distribution of 2# joint before and after the post-weld heat treatment
Samples | Tensile strength (MPa) | Elongation (%) | Elongation after fracture (%) |
---|---|---|---|
1-1# | 310 | 8.0 | 8.3 |
1-2# | 309 | 7.6 | 8.0 |
1-3# | 443 | 5.4 | 5.9 |
1-4# | 449 | 7.6 | 7.9 |
2-1# | 278 | 3.9 | 5.1 |
2-2# | 270 | 3.7 | 4.1 |
2-3# | 447 | 6.1 | 6.7 |
2-4# | 454 | 7.0 | 7.2 |
Table 5 Tensile properties of the welded joints
Samples | Tensile strength (MPa) | Elongation (%) | Elongation after fracture (%) |
---|---|---|---|
1-1# | 310 | 8.0 | 8.3 |
1-2# | 309 | 7.6 | 8.0 |
1-3# | 443 | 5.4 | 5.9 |
1-4# | 449 | 7.6 | 7.9 |
2-1# | 278 | 3.9 | 5.1 |
2-2# | 270 | 3.7 | 4.1 |
2-3# | 447 | 6.1 | 6.7 |
2-4# | 454 | 7.0 | 7.2 |
Fig. 12 True strain distributions on the edge surface under different stresses during the tensile test: a, b, c 1-1#, 1-3#, 1-4# specimens under stress of 300 MPa, respectively; d, e 1-3#, 1-4# specimens under stress of 430 MPa, respectively
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